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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-21 04:13:34 +08:00
Cleanup of lots of debugging printfs
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@@ -141,7 +141,6 @@ static int ardrone_open_uart(char *uart_name, struct termios *uart_config_origin
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int uart;
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/* open uart */
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//printf("[ardrone_interface] UART is %s, baud rate is%d\n",uart_name,speed);
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uart = open(uart_name, O_RDWR | O_NOCTTY);
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/* Try to set baud rate */
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@@ -238,15 +237,14 @@ int ardrone_interface_thread_main(int argc, char *argv[])
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/* declare and safely initialize all structs */
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struct vehicle_status_s state;
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//memset(&state, 0, sizeof(state));
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memset(&state, 0, sizeof(state));
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struct actuator_controls_s actuator_controls;
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//memset(&actuator_controls, 0, sizeof(actuator_controls));
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memset(&actuator_controls, 0, sizeof(actuator_controls));
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struct actuator_armed_s armed;
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armed.armed = false;
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/* subscribe to attitude, motor setpoints and system state */
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int actuator_controls_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS);
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int state_sub = orb_subscribe(ORB_ID(vehicle_status));
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int armed_sub = orb_subscribe(ORB_ID(actuator_armed));
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@@ -328,11 +326,6 @@ int ardrone_interface_thread_main(int argc, char *argv[])
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* if in failsafe
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*/
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if (armed.armed && !armed.lockdown) {
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//printf("AMO_BEF: Roll: %4.4f, Pitch: %4.4f, Yaw: %4.4f, Thrust: %4.4f\n",actuator_controls.control[0], actuator_controls.control[1], actuator_controls.control[2], actuator_controls.control[3]);
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ardrone_mixing_and_output(ardrone_write, &actuator_controls);
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} else {
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@@ -388,16 +388,12 @@ void ardrone_mixing_and_output(int ardrone_write, const struct actuator_controls
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if (motor_thrust <= min_thrust) {
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motor_thrust = min_thrust;
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output_band = 0.0f;
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//printf("0 silent\n");
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} else if (motor_thrust < startpoint_full_control && motor_thrust > min_thrust) {
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output_band = band_factor * (motor_thrust - min_thrust);
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//printf("1 starting\n");
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} else if (motor_thrust >= startpoint_full_control && motor_thrust < max_thrust - band_factor * startpoint_full_control) {
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output_band = band_factor * startpoint_full_control;
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//printf("2 working\n");
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} else if (motor_thrust >= max_thrust - band_factor * startpoint_full_control) {
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output_band = band_factor * (max_thrust - motor_thrust);
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//printf("3 full\n");
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}
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//add the yaw, nick and roll components to the basic thrust //TODO:this should be done by the mixer
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